| 摘要 |
<p>The invention relates to a device 1 for suspending a casing 2 of a turbine engine 3 to the structure 12 of an aircraft. The device 1 is characterized in that it comprises a suspension ring 4, the suspension ring 4 comprising: a plurality of attachment surfaces 33 positioned so as to protrude on the circumference of the suspension ring 4 and having attachment holes 6, for attachment to the structure 12; a circumferential flange 5 comprising a plurality of holes 35 for attaching the suspension ring 4 to the casing 2; and several hanging surfaces 10 for hanging at least one piece of equipment 15. The hanging surfaces 10 are positioned so as to protrude on the circumference of the suspension ring 4, and having holes 8 for hanging the piece of equipment 15 to the ring 4.The invention also relates to a turbine engine and to a propulsion assembly comprising such a device.</p> |
